CN116443253A - System and method for oxygen supply, heat supply and energy source of high-altitude airship - Google Patents
System and method for oxygen supply, heat supply and energy source of high-altitude airship Download PDFInfo
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- CN116443253A CN116443253A CN202310421325.6A CN202310421325A CN116443253A CN 116443253 A CN116443253 A CN 116443253A CN 202310421325 A CN202310421325 A CN 202310421325A CN 116443253 A CN116443253 A CN 116443253A
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- oxygen
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- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 title claims abstract description 43
- 239000001301 oxygen Substances 0.000 title claims abstract description 43
- 229910052760 oxygen Inorganic materials 0.000 title claims abstract description 43
- 238000000034 method Methods 0.000 title claims description 11
- 238000005868 electrolysis reaction Methods 0.000 claims abstract description 26
- 238000000746 purification Methods 0.000 claims abstract description 18
- 238000004146 energy storage Methods 0.000 claims abstract description 14
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 79
- 235000011089 carbon dioxide Nutrition 0.000 claims description 69
- 239000010410 layer Substances 0.000 claims description 29
- 238000003860 storage Methods 0.000 claims description 21
- 239000001257 hydrogen Substances 0.000 claims description 17
- 229910052739 hydrogen Inorganic materials 0.000 claims description 17
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 17
- 229910001868 water Inorganic materials 0.000 claims description 17
- 239000007789 gas Substances 0.000 claims description 12
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 11
- 238000005485 electric heating Methods 0.000 claims description 11
- 238000006243 chemical reaction Methods 0.000 claims description 10
- 239000007788 liquid Substances 0.000 claims description 9
- 238000010438 heat treatment Methods 0.000 claims description 8
- 150000002431 hydrogen Chemical class 0.000 claims description 6
- 239000011229 interlayer Substances 0.000 claims description 6
- 238000002360 preparation method Methods 0.000 claims description 6
- 230000015572 biosynthetic process Effects 0.000 claims description 5
- 229910002092 carbon dioxide Inorganic materials 0.000 claims description 5
- 239000001569 carbon dioxide Substances 0.000 claims description 5
- 238000012545 processing Methods 0.000 claims description 4
- 239000012535 impurity Substances 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 238000012544 monitoring process Methods 0.000 claims description 3
- 239000002912 waste gas Substances 0.000 claims description 3
- 230000007774 longterm Effects 0.000 claims description 2
- 238000010248 power generation Methods 0.000 abstract description 15
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000003595 mist Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000005192 partition Methods 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S10/00—PV power plants; Combinations of PV energy systems with other systems for the generation of electric power
- H02S10/10—PV power plants; Combinations of PV energy systems with other systems for the generation of electric power including a supplementary source of electric power, e.g. hybrid diesel-PV energy systems
- H02S10/12—Hybrid wind-PV energy systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D13/08—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25B—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES FOR THE PRODUCTION OF COMPOUNDS OR NON-METALS; APPARATUS THEREFOR
- C25B1/00—Electrolytic production of inorganic compounds or non-metals
- C25B1/01—Products
- C25B1/02—Hydrogen or oxygen
- C25B1/04—Hydrogen or oxygen by electrolysis of water
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25B—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES FOR THE PRODUCTION OF COMPOUNDS OR NON-METALS; APPARATUS THEREFOR
- C25B15/00—Operating or servicing cells
- C25B15/08—Supplying or removing reactants or electrolytes; Regeneration of electrolytes
- C25B15/085—Removing impurities
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25B—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES FOR THE PRODUCTION OF COMPOUNDS OR NON-METALS; APPARATUS THEREFOR
- C25B9/00—Cells or assemblies of cells; Constructional parts of cells; Assemblies of constructional parts, e.g. electrode-diaphragm assemblies; Process-related cell features
- C25B9/60—Constructional parts of cells
- C25B9/65—Means for supplying current; Electrode connections; Electric inter-cell connections
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/14—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0677—Environmental Control Systems comprising on board oxygen generator systems
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Electrochemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Materials Engineering (AREA)
- Pulmonology (AREA)
- Power Engineering (AREA)
- General Health & Medical Sciences (AREA)
- Health & Medical Sciences (AREA)
- Mechanical Engineering (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Life Sciences & Earth Sciences (AREA)
- Inorganic Chemistry (AREA)
- Electrolytic Production Of Non-Metals, Compounds, Apparatuses Therefor (AREA)
Abstract
The invention discloses an oxygen supply, heat supply and energy supply system for a high-altitude airship, which comprises a solar power generation module, a wind power generation module and an energy storage module, wherein the output end of the energy storage module is provided with an electrolysis module, the input end of the electrolysis module is provided with a purification module, and the oxygen supply, heat supply and power system for long-time operation of the high-altitude airship is created in the invention.
Description
Technical Field
The invention belongs to the technical field of energy systems, and particularly relates to a system and a method for oxygen supply, heat supply and energy of a high-altitude airship.
Background
The high-altitude unmanned airship is a novel near space aircraft, the flying height can reach 20km, the advantages of the high-altitude airship are obvious, the high-altitude unmanned airship can be repeatedly used, stays high for a long time, even reaches several months or longer, can execute various tasks such as early warning, reconnaissance, communication and the like, and has high-altitude travel value. Compared with an airplane, the aircraft has the advantages of being difficult to replace, low in cost and wide in development prospect. Because the air at high altitude is thin, the oxygen content is low, the temperature is also low, and the living environment in the airship can not meet the long-time living requirement by directly using the outside air. At present, extra oxygen can be carried to supply into the airship cabin through a special oxygen supply system, which needs to carry enough oxygen, and long-time high-altitude flight cannot be met due to limited load of the airship. The air supply system similar to an airplane is adopted, namely, external air is compressed and cooled through a power system and then supplied to the cabin, the mode can supply air with proper temperature for a long time, but the air supply system needs a complicated power compression system, has high energy consumption, and if the air supply system is used for supplying power for solar energy, the airship needs to carry a relatively large solar power generation system; in the case of a gas power system, more and heavier fuel needs to be carried to meet long-term flight, and the power system is relatively noisier.
Disclosure of Invention
The invention aims to provide a system and a method for oxygen supply, heat supply and energy sources of a high-altitude airship so as to solve the problem.
In order to achieve the above purpose, the present invention provides the following technical solutions: the system for supplying oxygen, heat and energy of the high-altitude airship comprises a solar power generation module, a wind power generation module and an energy storage module, wherein an electrolysis module is arranged at the output end of the energy storage module, a purification module is arranged at the input end of the electrolysis module, a formation module is arranged at the input end of the purification module, a dry ice module and a collection module are arranged at the input end of the formation module, and an exhaust module is arranged at the output end of the formation module;
the collecting module comprises a first shell and a second shell which are arranged on the airship, a collecting pipeline is arranged on the first shell, the bottom of the first shell is connected to an internal fan of the airship, arc-shaped guide grooves which can form an interlayer are formed in the arc-shaped guide grooves and the second shell, dry ice bins which can be replaced with each other are arranged in the interlayer, a power component is arranged between the dry ice bins, a dry ice storage cavity is arranged on the second shell, an electric valve is arranged on the dry ice storage cavity, the electric valve is arranged above one dry ice bin, a liquid receiving component is externally connected to the bottom of the first shell and the bottom of the second shell, and a heating component used for liquefying is arranged at the bottom of the dry ice bin in the second shell.
Preferably, the output end of the exhaust module is provided with a processing module, the output end of the purification module is provided with living equipment, and the output end of the electrolysis module is provided with oxygen storage equipment and hydrogen storage equipment.
Preferably, pressure sensors are arranged on the upper side and the lower side of the arc-shaped guide groove in the first shell, and a guide hole is formed in the dry ice bin.
Preferably, the power component comprises a motor arranged at the joint of the middle part of the arc-shaped guide groove, a rotating shaft is fixedly connected to an output shaft of the motor, lifting rods capable of being connected between the dry ice bin and the rotating shaft are fixedly connected to two sides of the rotating shaft, and springs are sleeved on the outer sides of the lifting rods.
Preferably, the heating element is including setting up in the inside dry ice storehouse bottom of second casing electrical heating board, electrical heating board bottom fixedly connected with link and arc guide way inner wall fixed connection.
Preferably, the baffle plate which can be used for the rotation replacement of the two dry ice bins is processed on the arc-shaped guide groove at the lower part, and the through hole with the same size as the opening at the top of the dry ice bin is formed on the arc-shaped guide groove at the upper part.
Preferably, the liquid receiving component comprises a diversion pipeline arranged at one side of the bottoms of the first shell and the second shell, a purifying box body is fixedly arranged at the rear sides of the first shell and the second shell, and the purifying box body is communicated with the inside of the first shell and the inside of the second shell through the diversion pipeline.
A method of operating a system for oxygen supply, heat supply and energy for a high-altitude airship, characterized by: the method comprises the following specific steps:
step one: the energy is stored in the energy storage device,
s1, solar energy and wind energy are generated and stored through a solar power generation module and a wind power generation module;
s2, generating hydrogen, oxygen and water by power supply equipment;
1. collecting, namely, by starting a fan in the airship and communicating the fan with the collecting pipeline through the first shell, the collecting pipeline can suck the external cloud layer until the external cloud layer is sucked into the first shell;
2. the formation, utilize the realization at the inside dry ice that sets up of two dry ice warehouses, can make the cloud that gathers and dry ice reaction, generate little raindrops, flow into the water conservancy diversion pipeline from the water conservancy diversion hole until flow to purification module inside:
the temperature is reduced due to the fact that raindrops are generated in the reaction between the dry ice and the cloud, an ice layer is formed for a long time to influence the circulation of gas and the diversion and collection of rainwater, at the moment, pressure difference is formed at two sides of a dry ice bin once the ice layer is formed to influence the circulation, a motor can be immediately started to rotate and replace the two dry ice bins when the pressure difference is generated by utilizing the monitoring of a pressure sensor, the ice layer generating one of the dry ice bins is moved to the top of an electric heating plate, the electric heating plate is started to melt the ice layer, the ice layer is removed from being blocked, and then the inside of the dry ice bin which is just rotated at the bottom of the ice bin is supplemented by utilizing an electric valve;
3. purifying, wherein the collected rainwater often contains impurities, and filtering and purifying are performed by using a purifying module, so that the water body meets the electrolysis requirement;
4. materials which are helpful for electrolysis can be added during the preparation, so that the electrolysis efficiency is improved;
5. electrolyzing, namely electrolyzing the liquid prepared by the preparation module by utilizing an electrolysis module to generate oxygen and hydrogen, and respectively storing the two gases by utilizing an oxygen storage device and a hydrogen storage device;
step two: and (3) treating waste gas, wherein carbon dioxide is generated by the reaction of dry ice and the collected cloud layer gas, and the carbon dioxide can be led into the treatment module through the exhaust module to be subjected to centralized treatment.
The invention has the technical effects and advantages that: the invention provides an oxygen supply, heat supply system and power system for long-time operation of the high-altitude airship, which are combined with a wind, solar power generation system and an electrolytic water hydrogen and oxygen generating system to supply energy for the airship, thereby reducing the carrying capacity of the airship and solving the problem that the airship flies in high altitude for a long time or even indefinitely;
the oxygen supply, heat supply system and power system for long-time operation of the high-altitude airship provided by the invention fully utilize the high-altitude flight environment of the airship, and the indefiniteness of the amounts of wind energy, solar energy, cloud and air is introduced into the water electrolysis hydrogen production gas system, so that the whole system can efficiently and continuously provide oxygen, heat and power requirements for the airship;
and the internal reaction after collection is designed according to the actual situation, then the regulation and control of the ice layer are carried out, after all, the water mist in the cloud layer is unfavorable for collection, and the dry ice is directly sprayed out to form large-scale rainfall, so that the collection of the maximum efficiency is unfavorable.
Drawings
FIG. 1 is a control system diagram of the present invention;
FIG. 2 is a block diagram of a receiving module according to the present invention;
FIG. 3 is a cross-sectional view of a collection module of the present invention;
FIG. 4 is an enlarged view of part A of FIG. 3 in accordance with the present invention;
fig. 5 is a schematic view of an arc-shaped guide groove structure of the present invention.
In the figure: 1. a dry ice module; 2. a collecting module; 201. a deflector aperture; 202. a dry ice bin; 203. an arc-shaped guide groove; 204. a pressure sensor; 205. a collection pipe; 206. a first housing; 207. a dry ice storage chamber; 208. an electric valve; 209. purifying the box body; 210. a diversion pipeline; 211. an electric heating plate; 212. a motor; 213. a rotating shaft; 214. a lifting rod; 215. a spring; 216. a partition plate; 217. a second housing; 3. forming a module; 4. an exhaust module; 5. a processing module; 6. living equipment; 7. an oxygen storage device; 8. a hydrogen storage device; 9. an electrolysis module; 10. an energy storage module; 11. a solar power generation module; 12. a wind power generation module; 13. and a purification module.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
The invention provides a system for supplying oxygen, heat and energy for a high-altitude airship, which is shown in the figure, and comprises a solar power generation module 11, a wind power generation module 12 and an energy storage module 10, wherein the output end of the energy storage module 10 is provided with an electrolysis module 9, the input ends of the electrolysis module 9 are provided with 14, the input ends of the 14 are provided with a purification module 13, the input end of the purification module 13 is provided with a forming module 3, the input end of the forming module 3 is provided with a dry ice module 1 and a collecting module 2, and the output end of the forming module 3 is provided with an exhaust module 4;
the collecting module 2 comprises a first shell 206 and a second shell 217 which are arranged on the airship, a collecting pipeline 205 is arranged on the first shell 206, the bottom of the first shell 206 is connected to an internal fan of the airship, an arc-shaped guide groove 203 capable of forming an interlayer is arranged inside the arc-shaped guide groove 203 and the second shell 217, a dry ice bin 202 capable of being replaced with each other is arranged in the interlayer, a power component is arranged between the two dry ice bins 202, a dry ice storage cavity 207 is arranged on the second shell 217, an electric valve 208 is arranged on the dry ice storage cavity 207, the electric valve 208 is arranged above one dry ice bin 202, a liquid receiving component is externally connected to the bottoms of the first shell 206 and the second shell 217, and a heating component for liquefying is arranged at the bottom of the dry ice bin 202 inside the second shell 217.
Specifically, the output of exhaust module 4 is provided with processing module 5, and the output of purification module 13 is provided with life equipment 6, and the output of electrolysis module 9 is provided with oxygen storage equipment 7 and hydrogen storage equipment 8.
Specifically, pressure sensors 204 are disposed on the upper and lower sides of the arc-shaped guide groove 203 in the first housing 206, and a guide hole 201 is formed in the dry ice bin 202.
Specifically, the power component includes motor 212 that sets up in arc guide slot 203 middle part junction, fixedly connected with pivot 213 on motor 212's the output shaft, the equal fixedly connected with of pivot 213 both sides is connected with the lift pole 214 that contracts between dry ice storehouse 202 and the pivot 213, and lift pole 214 outside cover is equipped with spring 215.
Specifically, the heating assembly includes an electric heating plate 211 disposed at the bottom of the dry ice bin 202 inside the second housing 217, and a connecting frame is fixedly connected to the bottom of the electric heating plate 211 and fixedly connected to the inner wall of the arc-shaped guide groove 203.
Specifically, a partition plate 216 for rotating and replacing the two dry ice bins 202 is processed on the lower arc-shaped guide groove 203, and a through hole with the same size as the opening at the top of the dry ice bin 202 is formed on the upper arc-shaped guide groove 203.
Specifically, the liquid receiving assembly includes a diversion pipeline 210 disposed at one side of the bottoms of the first casing 206 and the second casing 217, a purifying box 209 is fixedly disposed at the rear sides of the first casing 206 and the second casing 217, and the purifying box 209 is communicated with the inside of the first casing 206 and the second casing 217 through the diversion pipeline 210.
A method of operating a system for oxygen supply, heat supply and energy for a high-altitude airship, characterized by: the method comprises the following specific steps:
step one: the energy is stored in the energy storage device,
s1, solar energy and wind energy are generated through a solar power generation module 11 and a wind power generation module 12 and stored;
s2, generating hydrogen, oxygen and water by power supply equipment;
1. collecting, namely, by starting a fan in the airship and communicating the fan with the collecting pipeline 205 through the first shell 206, the collecting pipeline 205 can suck the external cloud layer until the external cloud layer is sucked into the first shell 206;
2. by forming the dry ice inside the two dry ice bins 202, the collected dry ice can react with the dry ice to generate small raindrops, and the small raindrops flow from the diversion holes 201 into the diversion pipeline 210 until flowing into the purification module 13:
the temperature is reduced due to the reaction of generating raindrops between the dry ice and the cloud, an ice layer is formed for a long time to influence the circulation of gas and the diversion and collection of rainwater, at the moment, pressure difference is formed at two sides of the dry ice bin 202 once the ice layer is formed to influence the circulation, the motor 212 can be immediately started to rotate and replace the two dry ice bins 202 by utilizing the monitoring of the pressure sensor 204 when the pressure difference is generated, the ice layer generating one is moved to the top of the electric heating plate 211, meanwhile, the electric heating plate 211 is started to melt the ice layer, the ice layer blockage is relieved, and then the electric valve 208 is utilized to supplement dry ice in the dry ice bin 202 which is just rotated at the bottom of the ice layer;
the conversion between the two dry ice bins 202 is realized by driving the rotating shaft 213 to rotate through the motor 212 so as to drive the two dry ice bins 202 to rotate and replace through the two lifting rods 214, and the cooperation between the lifting rods 214 and the springs 215 through the arc-shaped guide grooves can maximally reduce the whole shell volume, reduce the waste space and reset through the guide compression springs;
3. the collected rainwater is always polluted by impurities, and the water is filtered and purified by the purification module 13, so that the water body is more in line with the electrolysis requirement;
4. materials which are helpful for electrolysis can be added during the preparation, so that the electrolysis efficiency is improved;
5. electrolyzing, namely electrolyzing the liquid prepared by the preparation module by utilizing an electrolysis module 9 to generate oxygen and hydrogen, and respectively storing the two gases by utilizing an oxygen storage device 7 and a hydrogen storage device 8;
step two: waste gas treatment, in which carbon dioxide is generated by the reaction of dry ice and the collected cloud layer gas and can be led into the treatment module 5 through the exhaust module 4 for centralized treatment;
the invention provides an oxygen supply, heat supply system and power system for long-time operation of the high-altitude airship, which are combined with a wind, solar power generation system and an electrolytic water hydrogen and oxygen generating system to supply energy for the airship, thereby reducing the carrying capacity of the airship and solving the problem that the airship flies in high altitude for a long time or even indefinitely;
the oxygen supply, heat supply system and power system for long-time operation of the high-altitude airship provided by the invention fully utilize the high-altitude flight environment of the airship, and the indefiniteness of the amounts of wind energy, solar energy, cloud and air is introduced into the water electrolysis hydrogen production gas system, so that the whole system can efficiently and continuously provide oxygen, heat and power requirements for the airship;
and the internal reaction after collection is designed according to the actual situation, then the regulation and control of the ice layer are carried out, after all, the water mist in the cloud layer is unfavorable for collection, and the dry ice is directly sprayed out to form large-scale rainfall, so that the collection of the maximum efficiency is unfavorable.
Finally, it should be noted that: the foregoing description is only illustrative of the preferred embodiments of the present invention, and although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described, or equivalents may be substituted for elements thereof, and any modifications, equivalents, improvements or changes may be made without departing from the spirit and principles of the present invention.
Claims (8)
1. A system for oxygen supply, heat supply and energy supply of a high-altitude airship, comprising a solar power module (11), a wind power module (12) and an energy storage module (10), characterized in that: the energy storage device comprises an energy storage module (10), wherein an electrolysis module (9) is arranged at the output end of the energy storage module (10), a purification module (13) is arranged at the input end of the electrolysis module (9), a forming module (3) is arranged at the input end of the purification module (13), a dry ice module (1) and a collecting module (2) are arranged at the input end of the forming module (3), and an exhaust module (4) is arranged at the output end of the forming module (3);
the collecting module (2) comprises a first shell (206) and a second shell (217) which are arranged on the airship, a collecting pipeline (205) is arranged on the first shell (206), the bottom of the first shell (206) is connected to an internal fan of the airship, an arc-shaped guide groove (203) capable of forming an interlayer is arranged inside the arc-shaped guide groove (203) and the second shell (217), a dry ice bin (202) capable of being replaced with each other is arranged in the interlayer, a power assembly is arranged between the dry ice bins (202), a dry ice storage cavity (207) is arranged on the second shell (217), an electric valve (208) is arranged on the dry ice storage cavity (207), a liquid receiving assembly is externally connected to the bottoms of the first shell (206) and the second shell (217), and a heating assembly for liquefying is arranged at the bottom of the dry ice bin (202) inside the second shell (217).
2. A system for oxygen supply, heat supply and energy for high altitude airships according to claim 1, wherein: the output end of the exhaust module (4) is provided with a processing module (5), the output end of the purification module (13) is provided with a living device (6), and the output end of the electrolysis module (9) is provided with an oxygen storage device (7) and a hydrogen storage device (8).
3. A system for oxygen supply, heat supply and energy for high altitude airships according to claim 1, wherein: pressure sensors (204) are arranged on the upper side and the lower side of an arc-shaped guide groove (203) in the first shell (206), and a guide hole (201) is formed in the dry ice bin (202).
4. A system for oxygen supply, heat supply and energy for high altitude airships according to claim 1, wherein: the power assembly comprises a motor (212) arranged at the joint of the middle part of the arc-shaped guide groove (203), a rotating shaft (213) is fixedly connected to an output shaft of the motor (212), lifting rods (214) capable of being connected between the dry ice bin (202) and the rotating shaft (213) are fixedly connected to two sides of the rotating shaft (213), and springs (215) are sleeved on the outer sides of the lifting rods (214).
5. A system and method for oxygen supply, heat supply and energy for high altitude airships according to claim 1, wherein: the heating assembly comprises an electric heating plate (211) arranged at the bottom of the dry ice bin (202) inside the second shell (217), and a connecting frame is fixedly connected to the bottom of the electric heating plate (211) and fixedly connected with the inner wall of the arc-shaped guide groove (203).
6. A system for oxygen supply, heat supply and energy for high altitude airships according to claim 1, wherein: the lower part of the arc-shaped guide groove (203) is provided with a baffle plate (216) which can be used for rotating and replacing the two dry ice bins (202), and the upper part of the arc-shaped guide groove (203) is provided with a through hole with the same size as the opening at the top of the dry ice bins (202).
7. A system for oxygen supply, heat supply and energy for high altitude airships according to claim 1, wherein: the liquid receiving component comprises a diversion pipeline (210) arranged at one side of the bottoms of the first shell (206) and the second shell (217), a purification box body (209) is fixedly arranged at the rear side of the first shell (206) and the second shell (217), and the purification box body (209) is communicated with the inside of the first shell (206) and the inside of the second shell (217) through the diversion pipeline (210).
8. A method of operating a system for supplying oxygen, heat and energy for long term operation of an overhead airship according to claim 1, wherein: the method comprises the following specific steps:
step one: the energy is stored in the energy storage device,
s1, solar energy and wind energy are generated and stored through a solar energy generation module (11) and a wind energy generation module (12);
s2, generating hydrogen, oxygen and water by power supply equipment;
1. collecting, namely, by starting a fan in the airship and communicating the fan with the collecting pipeline (205) through the first shell (206), the collecting pipeline (205) can suck the external cloud layer until the external cloud layer is sucked into the first shell (206);
2. the formation, with the realization of the dry ice that sets up in two dry ice warehouses (202) inside, can make the cloud that gathers react with dry ice, produces little raindrops, flows into guide pipeline (210) from water conservancy diversion hole (201) until flow to purification module (13) inside:
the temperature is reduced due to the fact that raindrops are generated in the reaction between the dry ice and the cloud, an ice layer is formed for a long time to influence the circulation of gas and the diversion and collection of rainwater, at the moment, pressure difference is formed at two sides of the dry ice bin (202) once the ice layer is formed to influence the circulation, the pressure sensor (204) is used for monitoring, when the pressure difference is generated, a motor (212) can be immediately started to rotate and replace the two dry ice bins (202), the ice layer is moved to the top of an electric heating plate (211), the electric heating plate (211) is started to melt the ice layer, the ice layer is removed from being blocked, and then the inside of the dry ice bin (202) which is just rotated at the bottom of the ice bin is supplemented by an electric valve (208);
3. the collected rainwater is always polluted by impurities, and the water is filtered and purified by the purification module (13) so that the water body meets the electrolysis requirement;
4. materials which are helpful for electrolysis can be added during the preparation, so that the electrolysis efficiency is improved;
5. electrolyzing, namely electrolyzing the liquid prepared by the preparation module by utilizing an electrolysis module (9) to generate oxygen and hydrogen, and respectively storing the two gases by utilizing an oxygen storage device (7) and a hydrogen storage device (8);
step two: and (3) treating waste gas, wherein carbon dioxide is generated by the reaction of dry ice and the collected cloud layer gas, and the carbon dioxide can be introduced into the treatment module (5) through the exhaust module (4) to be intensively treated.
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